49.025.50 粘合剂 标准查询与下载

ASTM F942-18(2023)e1 航空航天透明外壳夹层材料试验方法选择的标准指南

1.1 This guide summarizes the standard test methods available for determining physical and mechanical characteristics of interlayer materials used in multi-ply aerospace transparent enclosures. 1.2 Interlayer materials are used to laminate glass-to-glass, glass-to-plastic, and plastic-to-plastic. Interlayer materials are basically transparent adhesives with high-quality optical properties. They can also serve as an energy absorbing medium, a fail-safe membrane to contain cockpit pressure and to prevent entry of impact debris; a strain insulator to accommodate different thermal expansion rates of members being laminated and as an adherent to prevent spalling of inner surface ply material fragments. The relative importance of an interlayer characteristic will be a function of the prime use it serves in its particular application. 1.3 This guide, as a summary of various methods in Section 2, is intended to facilitate the selection of tests that can be applied to interlayer materials. 1.4 The test methods listed are for use in determining basic design characteristics and in assuring lot-to-lot uniformity of the materials being tested except as noted in 3.3. 1.5 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety, health, and environmental practices and determine the applicability of regulatory limitations prior to use. 1.6 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.

Standard Guide for Selection of Test Methods for Interlayer Materials for Aerospace Transparent Enclosures

T/NXCL 010-2021 低温固化型银导体浆料

本文件规定了低温固化型银导体浆料的分类、技术要求、试验方法、检验规则和包装、标志、运输、贮存。本文件适用于薄膜开关及柔性印刷电路用银浆料、浸渍型钽电容器用银浆料、以及银导电胶等低温固化型银导体浆料。

Low temperature curing silver conductor paste

ASTM D6412/D6412M-99(2020) 用于粘结金属和非金属材料的环氧（柔性）粘合剂的标准规范

1.1 The specification covers a two-part modified epoxy paste adhesive for bonding metallic and nonmetallic materials. The adhesive should be suitable for forming bonds that can withstand environmental exposure to temperatures from –184 to 82 °C [–300 to 180 °F] when exposed to an expected combination of stress, temperature, and relative humidity to be encountered in service. NOTE 1—When coordinated through the Department of Defense (DoD) and the National Aeronautics and Space Administration (NASA), this practice will be a direct replacement of MIL-A-82720 (OS), MIS-26872, and MSFC-SPEC-2037. 1.2 The values stated in SI units or inch-pound units are to be regarded separately as standard. Within the text, the inch-pound units are shown in brackets. The values stated in each system are not exact equivalents; therefore, each system must be used independently of the other. Combining values from the two systems may result in nonconformance with this specification. 1.3 The following precautionary statement pertains to the test method portion only, Section 8, of this specification: This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety, health, and environmental practices and determine the applicability of regulatory limitations prior to use. 1.4 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.

Standard Specification for Epoxy (Flexible) Adhesive For Bonding Metallic And Nonmetallic Materials

BS EN 2667-3:2019 航空航天系列 非金属材料 发泡结构粘合膜 测试方法-膨胀率和挥发物含量

What is BS EN 2667-3- Aerospace series: Foaming structural adhesive films about?   BS EN 2667-3 is a standard that covers technical specifications for the Aerospace series: structural foaming adhesive films that ensure advanced bonding and fire resistance in aerospace applications.   BS EN 2667-3 specifies the test method for determining the expansion ratio and the volatile content in structural foaming adhesive films.   Who is BS EN 2667-3- Aerospace series: Foaming structural adhesive films for?   BS EN 2667-3 on aerospace series: Foaming structural adhesive films applies to:   Manufacturers of adhesive films  

Aerospace series. Non-metallic materials. Foaming structural adhesive films. Test methods - Expansion ratio and volatile content

ASTM F942-18 航空航天透明罩内层材料试验方法选择标准指南

1.1 This guide summarizes the standard test methods available for determining physical and mechanical characteristics of interlayer materials used in multi-ply aerospace transparent enclosures. 1.2 Interlayer materials are used to laminate glass-to-glass, glass-to-plastic, and plastic-to-plastic. Interlayer materials are basically transparent adhesives with high-quality optical properties. They can also serve as an energy absorbing medium, a fail-safe membrane to contain cockpit pressure and to prevent entry of impact debris; a strain insulator to accommodate different thermal expansion rates of members being laminated and as an adherent to prevent spalling of inner surface ply material fragments. The relative importance of an interlayer characteristic will be a function of the prime use it serves in its particular application. 1.3 This guide, as a summary of various methods in Section 2, is intended to facilitate the selection of tests that can be applied to interlayer materials. 1.4 The test methods listed are for use in determining basic design characteristics and in assuring lot-to-lot uniformity of the materials being tested except as noted in 3.3. 1.5 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety, health, and environmental practices and determine the applicability of regulatory limitations prior to use. 1.6 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.

Standard Guide for Selection of Test Methods for Interlayer Materials for Aerospace Transparent Enclosures

BS EN 2667-2:2018 航空航天系列. 非金属材料. 发泡结构胶. 试验方法. 压管剪

Aerospace series. Non-metallic materials. Foaming structural adhesives. Test methods. Compressive tube shear

EN 2667-2:2018 航空航天系列非金属材料发泡结构胶试验方法第2部分：压缩管剪切

Aerospace series - Non-metallic materials - Foaming structural adhesives - Test methods - Part 2: Compressive tube shear

SAE AMS3809A-2015 胶带，粘性，压敏，双面，地毯捆绑

This specification covers a fabric in the form of a double-faced, pressure-sensitive, adhesive tape.

Tape, Adhesive, Pressure-Sensitive, Double-Faced, Carpet Tie Down

SAE AMS2980/5A-2014 碳纤维织物和环氧树脂湿浸渍增强修复材料.第5部分:材料规范:平织、193 g/m²环氧和碳纤维织物

This Material Specification defines the requirements of carbon fiber fabric and epoxy resin systems used for wet lay-up repair of carbon fiber reinforced epoxy structures, qualified according to AMS 2980/1 and 2980/2.

Carbon Fiber Fabric and Epoxy Resin Wet Lay-Up Repair Material Part 5 - Material Specification: Carbon Fiber Fabrics, Plain Weave, 193 g/m2, and Epoxy Resin

SAE AMS2980/2B-2014 技术规范:碳纤维织物和环氧树脂湿浸渍增强修复材料.第2部分:合格鉴定计划

AMS 2980/2 gives specific information about the qualification program for carbon fiber fabric, epoxy systems and the material combination used for wet lay-up repair of carbon fiber reinforced epoxy structures.

Technical Specification: Carbon Fiber Fabric and Epoxy Resin Wet Lay-Up Repair Material Part 2 - Qualification Program

SAE AMS2980/1B-2014 技术规范:碳纤维织物和环氧树脂湿浸渍增强修复材料.第1部分:一般要求

AMS 2980/1 gives information about the technical requirements and qualification procedure for carbon fiber fabric and epoxy resin systems used for wet lay-up repair of carbon fiber reinforced epoxy structures.

Technical Specification: Carbon Fiber Fabric and Epoxy Resin Wet Lay-Up Repair Material Part 1 - General Requirements

SAE AMS2980/3B-2014 技术规范:碳纤维织物和环氧树脂湿浸渍增强修复材料采购规范.织物

The PS specifies the batch release and delivery requirements for carbon fiber and carbon fabric used for wet lay-up repair purposes.

Technical Specification: Carbon Fiber Fabric and Epoxy Resin Wet Lay-Up Repair Material Purchasing Specification - Fabric

SAE AMS2980/4B-2014 技术规范:碳纤维织物和环氧树脂湿浸渍增强修复材料采购规范.树脂

This PS specifies the batch release and delivery requirements for epoxy resin systems (base resin and curing agent) used for wet lay-up repair purposes.

Technical Specification: Carbon Fiber Fabric and Epoxy Resin Wet Lay-Up Repair Material Purchasing Specification - Resin

SAE AMS2980B-2014 技术规范:碳纤维织物和环氧树脂潮湿堆积修复材料.第0部分:介绍

This document (Technical Specification) gives information about qualification rules and the relation between the different specification parts involved, such as Technical Specification (TS), Material Specification (MS), and Purchasing Specification (PS). The link to material qualification and qualified products is presented.

Technical Specification: Carbon Fiber Fabric and Epoxy Resin Wet Lay-Up Repair Material, Part 0 - Introduction

NF L17-021*NF EN 4492:2013 航空航天系列.非金属材料.厌氧乳化剂化合物.螺纹锁.扭矩强度19 Nm

Aerospace series - Non-metallic materials - Anaerobic polymerisable compounds - Threadlocking - Torque strength 19 Nm

NF L17-313*NF EN 4106:2013 航空航天系列.非金属材料.结构型胶黏剂系统.糊状胶粘剂.技术规范

Aerospace series - Non-metallic materials - Structural adhesive systems - Paste adhesive - Technical specification

DIN EN 4491:2013 航空航天系列. 非金属材料. 厌氧可聚合化合物. 螺纹锁固. 抗扭强度16 Nm; 德文和英文版本EN 4491-2013

Aerospace series - Non-metallic materials - Anaerobic polymerisable compounds - Threadlocking - Torque strength 16 Nm; German and English version EN 4491:2013

DIN EN 4106:2013 航空航天系列. 非金属材料. 结构型粘合系统. 糊状粘合剂. 技术规范; 德文和英文版本EN 4106-2013

Aerospace series - Non-metallic materials - Structural adhesive systems - Paste adhesive - Technical specification; German and English version EN 4106:2013

DIN EN 4492:2013 航空航天系列.非金属材料.厌氧聚合物.螺纹锁.扭矩强度19 Nm.德文和英文版本EN 4492-2013

Aerospace series - Non-metallic materials - Anaerobic polymerisable compounds - Threadlocking - Torque strength 19 Nm; German and English version of EN 4492:2013

DIN EN 4488:2013 航空航天系列.非金属材料.厌氧乳化剂化合物.螺纹锁.扭矩强度2 Nm.德文和英文版本EN 4488-2013

Aerospace series - Non-metallic materials - Anaerobic polymerisable compounds - Threadlocking - Torque strength 2 Nm; German and English version EN 4488:2013